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JPS58202642A - Space diversity receiver - Google Patents

Space diversity receiver

Info

Publication number
JPS58202642A
JPS58202642A JP57084953A JP8495382A JPS58202642A JP S58202642 A JPS58202642 A JP S58202642A JP 57084953 A JP57084953 A JP 57084953A JP 8495382 A JP8495382 A JP 8495382A JP S58202642 A JPS58202642 A JP S58202642A
Authority
JP
Japan
Prior art keywords
station
receiver
space diversity
slave
master station
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP57084953A
Other languages
Japanese (ja)
Other versions
JPS6343027B2 (en
Inventor
Kazuhiro Yamamoto
和弘 山本
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NEC Corp
Original Assignee
NEC Corp
Nippon Electric Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by NEC Corp, Nippon Electric Co Ltd filed Critical NEC Corp
Priority to JP57084953A priority Critical patent/JPS58202642A/en
Priority to US06/494,116 priority patent/US4530087A/en
Priority to DE8383105029T priority patent/DE3362522D1/en
Priority to AU14819/83A priority patent/AU561492B2/en
Priority to CA000428598A priority patent/CA1203646A/en
Priority to EP83105029A priority patent/EP0095165B1/en
Publication of JPS58202642A publication Critical patent/JPS58202642A/en
Publication of JPS6343027B2 publication Critical patent/JPS6343027B2/ja
Granted legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B7/00Radio transmission systems, i.e. using radiation field
    • H04B7/14Relay systems
    • H04B7/15Active relay systems
    • H04B7/185Space-based or airborne stations; Stations for satellite systems
    • H04B7/1851Systems using a satellite or space-based relay
    • H04B7/18513Transmission in a satellite or space-based system
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04LTRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L1/00Arrangements for detecting or preventing errors in the information received
    • H04L1/02Arrangements for detecting or preventing errors in the information received by diversity reception
    • H04L1/06Arrangements for detecting or preventing errors in the information received by diversity reception using space diversity

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Radio Relay Systems (AREA)
  • Radio Transmission System (AREA)
  • Time-Division Multiplex Systems (AREA)
  • Mobile Radio Communication Systems (AREA)

Abstract

PURPOSE:To enable the use even in a section inferior in propagation condition for a space diversity receiver which is provided to a master station in a time division multi-direction communication network, by monitoring the error factor of a demodulated signal independently in response to each slave station to perform the switch selection control. CONSTITUTION:A master station 100 contains conflict counting circuits 4 in numbers equal to slave sations A, B-H which require diversity. For instance, the burst receiving signal supplied from the sation A is received through a main antenna MA and a secondary antenna SA of the station 100 and demodulated by each receiver 2. The error pulses EP given from receivers 2 are counted by the circuit 4 for station A for the burst time during which the signals are received from the station A. The circuit 4 performs a control so that a signal switch 3 selects the receiving signal side having a better code error factor. When the burst time of the station A elapses, the circuit 4 holds its state and then restarts its function at the burst time of the station A after opening gates 5 and 6. The same operation is carried out also with other slave stations B-H.

Description

【発明の詳細な説明】 本発明は、散在する多数の子局と共通の一つの親局とで
形成される時分割多方向通信網におけるスペースダイパ
ーシティ方式に関し、特に。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates in particular to a space diversity system in a time division multidirectional communication network formed by a large number of scattered slave stations and a common master station.

親局に備えられるスペースダイパーシティ受信装置に関
するものである。
The present invention relates to a space diversity receiving device provided in a master station.

第1図を参照すると1本発明を適用する時分開学方向通
信方式が示されている。親局100からは時分割多重化
された信号全複数の子局A。
Referring to FIG. 1, there is shown a time/minute opening direction communication system to which the present invention is applied. The master station 100 sends time-division multiplexed signals to a plurality of slave stations A.

B、・・・、Hに対して一斉に連続モードで送信する。B, . . . , H are transmitted all at once in continuous mode.

一方、各子局は親局クロックと同期し、自局に割り当て
られた時間帯に親局へ向けてノ(−スト状に送信を行い
、親局において各子局からの)く−スト信号が時間軸上
で整然と並ぶようにしているため、親局のクロックによ
り簡単に識別再生することができる。
On the other hand, each slave station is synchronized with the master station's clock and transmits a signal in a stream to the master station during the time period assigned to it. Since the signals are arranged in an orderly manner on the time axis, they can be easily identified and reproduced using the master station's clock.

かかる時分割多方向通信網において、親局と子局の伝播
路が長距離あるいは海上伝播である場合にスペースダイ
パーシティを適用し回線品質を改善する必要がある。
In such a time-division multidirectional communication network, when the propagation path between the master station and the slave stations is long distance or ocean propagation, it is necessary to apply space diversity to improve line quality.

一方、2地点間の通信を目的とした対向回線のスペース
ダイパーシティ方式としては、第2図に示すように、主
アンテナMA及び副アンテナS’Aからの受信信号を各
々復調再生し、どちらか符号誤り率の少ない方の復調信
号を切替選択するベースバンド切替方式がある。第2図
において、1は送信機、2は主アンテナMAあるいは副
アンテナSAからの信号を受信し復調信号全出力すると
ともに復調信号の符号誤りを検出して誤りパルスEPi
出力する受信機、3は各受信機で復調されたベースバン
ド信号を切替える信号切替器、そして4は2台の受信機
2よりの誤りパルスEPヲ受は信号切替器3に誤り率の
少ない側の復調信号を選択させる切替制御信号CSヲ作
る競合計数回路である。
On the other hand, as shown in Fig. 2, in the space diversity method of opposing lines for the purpose of communication between two points, the received signals from the main antenna MA and the sub antenna S'A are each demodulated and regenerated. There is a baseband switching method that switches and selects a demodulated signal with a lower bit error rate. In Fig. 2, 1 is a transmitter, and 2 is a transmitter that receives a signal from the main antenna MA or auxiliary antenna SA, outputs the entire demodulated signal, detects a code error in the demodulated signal, and generates an error pulse EPi.
3 is a signal switcher that switches the baseband signal demodulated by each receiver, and 4 is a signal switcher 3 that receives the error pulse EP from the two receivers 2, and switches the side with a lower error rate to the signal switcher 3. This is a competition counting circuit that generates a switching control signal CS that selects the demodulated signal.

しかし、第2図のベースバンド切替方式を前記多方向通
信システムにそのまま適用すると。
However, if the baseband switching method shown in FIG. 2 is applied as is to the multidirectional communication system.

複数の子局の信号を受信している親局では、各子局ごと
に独立に回線状態全監視し制御することができず、十分
なスペースダイパーシティ効果が得られないという欠点
がある。
A master station receiving signals from a plurality of slave stations has the disadvantage that it cannot fully monitor and control the line status of each slave station independently, and a sufficient space diversity effect cannot be obtained.

本発明の目的は、第1図のような時分割多方向通信網に
おける親局に備えられるスペースダイパーシティ受信装
置において、各子局対応に独立に復調信号の誤)率を監
視し切替選択制御するスペースダイパーシティ受信装置
を提供し。
An object of the present invention is to independently monitor the error rate of demodulated signals for each slave station and control switching selection in a space diversity receiving device provided in a master station in a time-division multidirectional communication network as shown in Fig. 1. Provides a space-diaperity receiving device.

上記欠点を除去することにある。The purpose is to eliminate the above drawbacks.

3− 次に本発明の実施例について図面を参照して説明する。3- Next, embodiments of the present invention will be described with reference to the drawings.

第3図は本発明のスペースダイパーシティ方式の実施例
である。第6図において、4は競合計数回路であり、ダ
イパーシティの必要な子局A、 B、・・・、Hの数だ
け親局100に実装される。
FIG. 3 is an embodiment of the space diversity method of the present invention. In FIG. 6, reference numeral 4 denotes a competition counting circuit, which is installed in the master station 100 in the number of slave stations A, B, . . . , H that require diversity.

5は競合計数回路4に入力する受信機2からの誤りパル
スEPi各子局の信号を受信している時間帯だけ計数す
るようにバーストタイミングパルスBTPによりゲーi
かける第1のゲート回路、6は信号切替器3を制御する
競合計数回路出力の制御信号C8金、同じく各子局の信
号を受信している時間帯だけ出力させるだめの第2のゲ
ート回路である。なお、子局A、 B、・・・、Hの各
々に対応したバーストタイミングノくルスBTPA、 
BTP、・・・ BTPHはタイミング信号のマスター
である親局100の信号処理回路内のタイミングジェネ
レータ回路(図示せず)から供給される。
5 is an error pulse EPi from the receiver 2 which is input to the contention counting circuit 4. The burst timing pulse BTP is used to count the error pulses EPi from the receiver 2 so as to count only the time periods when signals from each slave station are being received.
The first gate circuit 6 is used to output the control signal C8 of the contention counting circuit output that controls the signal switch 3, and the second gate circuit is also used to output the control signal C8 only during the time period when each slave station's signal is being received. be. In addition, burst timing nodes BTPA, corresponding to each of slave stations A, B, ..., H,
BTP, . . . BTPH are supplied from a timing generator circuit (not shown) in the signal processing circuit of the master station 100, which is a timing signal master.

以上の構成により9例えばA局からのノ(−ス4− ト受信信号は親局100の主アンテナMA及び副アンテ
ナSAで受信され、各受信機2で復調される。一方、各
受信機2からの誤りパルスEPはA局からの信号を受信
しているバースト時間の間だけA局用競合計数回路4に
入力され、カウントされる。そして、このA局用競合計
数回路4は、信号切替器6に符号誤り率の良い受信信号
側を選択させるように制御する。A局のバースト時間が
過ぎると競合計数回路4ばその状態を保持し、再びA局
のバースト時間になるとその機能をゲート5及び6″f
f:開いて再開する。
With the above configuration, a node reception signal from station A, for example, is received by the main antenna MA and sub antenna SA of the master station 100, and demodulated by each receiver 2.On the other hand, each receiver 2 The error pulse EP from the station A is input to the contention counting circuit 4 for the A station and counted only during the burst time when the signal from the A station is being received. When the burst time of station A has passed, the contention counting circuit 4 maintains that state, and when the burst time of station A comes again, it gates its function. 5 and 6″f
f: Open and resume.

同様にダイパーシティの必要なり局についてもB局のバ
ースト時間の間、B局用競合計数回路を動作させB局に
対するベースバンド信号の切替を行う。なお、ダイパー
シティの不要な子局に対しては競合計数回路を持つ必要
はなく、固定的にどちらかの受信機の復調信号を選択す
るようにする。
Similarly, for stations that require diversity, the B-station contention counting circuit is operated during the B-station burst time to switch the baseband signal for the B-station. Note that it is not necessary to provide a competition counting circuit for slave stations that do not require diversity, and the demodulated signal of one of the receivers is fixedly selected.

第6図は子局A−Hの送信系を、親局100のダイパー
シティ受信系を示しているが、子局の受信系は連続モー
ドで受信するため、子局の受信系及び親局の送信系には
第2図で示した従来のダイパーシティ方式が適用できる
。このようにして、親局とスペースダイバーシティカ必
要となる子局との間に相方向のダイパーシティ・システ
ムが構成できる。
Figure 6 shows the transmission systems of the slave stations A-H and the diversity reception system of the master station 100, but since the reception systems of the slave stations receive in continuous mode, the reception systems of the slave stations and the diversity reception system of the master station are The conventional diversity method shown in FIG. 2 can be applied to the transmission system. In this way, a bidirectional diversity system can be constructed between the master station and the slave stations that require space diversity.

第4図はゲート回路5,6.競合計数回路4の具体的な
構成例で1図中、7flNビツトの計数回路で、Nの値
は切替までの検出時間を考慮して適当な値が決められる
。第5図は受信機2の具体的な構成例で、受信機2ば、
受信信号R8を受け、バースト信号の復調信号DATA
 ’jz出力する復調回路8と、徂規の識別器9と9作
為的に誤り率を悪くさせた識別器10と、識別器9゜1
0の出力を比較し、誤りパルスEPi発生させる比較器
11とにより構成されている。誤り率が劣化し始めると
、識別器1・0の出力が誤り始め、比較器11の出力に
誤シパルスが発生し。
FIG. 4 shows gate circuits 5, 6. A specific example of the configuration of the competition counting circuit 4 is shown in FIG. 1, which is a 7flN bit counting circuit, and the value of N is determined to be an appropriate value in consideration of the detection time until switching. FIG. 5 shows a specific example of the configuration of the receiver 2.
Upon receiving the received signal R8, demodulated signal DATA of the burst signal is received.
'jz output demodulation circuit 8, a customary discriminator 9, a discriminator 10 whose error rate is artificially made worse, and a discriminator 9゜1
The comparator 11 compares the outputs of 0 and generates an error pulse EPi. When the error rate starts to deteriorate, the outputs of the discriminators 1 and 0 start to be erroneous, and an erroneous pulse occurs in the output of the comparator 11.

回線品質の劣化を予測切替できる。Can predict deterioration in line quality.

以上説明したように本発明によれば、パース実現でき、
海上伝播など伝播条件の悪い区間にも多方向通信システ
ムを導入することが可能になる。
As explained above, according to the present invention, parsing can be realized,
This makes it possible to introduce a multi-directional communication system even in sections with poor propagation conditions, such as propagation by sea.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明が適用される時分割多方向通信方式を説
明するための図、第2図は従来のスペースダイパーシテ
ィ方式を示す図、第3図は本発明の一実施例を示す図、
第4図は第3図の競合計数回路4とゲート回路5及び6
との具体的な構成例を示す回路図、第5図は第3図の受
信機2の具体的構成例を示す回路図である。 100・・・親局、A−H・・・子局、1・・・送信機
、2・・・受信機、 MA・・・主アンテナ、 SA・
・・副アンテナ6・・・信号切替器、4・・−競合計数
回路、5・・・第1のゲート回路、6・・・第2のゲー
ト回路、7・・・計数回路、8・・・復調回路、9及び
10・・・識別器。 11・・・比較器、 EP・・・誤9パルス、 BTP
・・・バーストタイミングパルス、C8・・・制御信号
。 序1図
FIG. 1 is a diagram for explaining a time-division multidirectional communication system to which the present invention is applied, FIG. 2 is a diagram showing a conventional space diversity system, and FIG. 3 is a diagram illustrating an embodiment of the present invention. ,
Figure 4 shows the competition counting circuit 4 and gate circuits 5 and 6 in Figure 3.
FIG. 5 is a circuit diagram showing a specific example of the configuration of the receiver 2 in FIG. 3. 100... Master station, A-H... Slave station, 1... Transmitter, 2... Receiver, MA... Main antenna, SA.
...Sub antenna 6...Signal switcher, 4...-Conflict counting circuit, 5...First gate circuit, 6...Second gate circuit, 7...Counting circuit, 8... - Demodulation circuit, 9 and 10... discriminator. 11...Comparator, EP...False 9 pulses, BTP
... Burst timing pulse, C8... Control signal. Preface 1

Claims (1)

【特許請求の範囲】 1、複数の子局と一つの親局とにより通信網が形成され
、各子局は自局に割り当てられた時間帯に親局に向けて
送信し、親局は各子局からのバースト信号を受信する時
分割多方向通信システムにおける親局に備えられるスペ
ースダイパーシティ受信装置において、前記スペースダ
イパーシティ受信装置は、主アンテナを備えた第1の受
信機と、副アンテナを備えた第2の受信機とを有し、第
1及び第2の受信機は、それぞれ。 アンテナからの入力信号を復調する復調手段と。 復調した信号の符号誤りを検出し、誤りパルスを発生す
る検出手段とを有し、前記スペースダイパーシティ受信
装置は、さらに、スペースダイパーシティを必要とする
各子局ごとに設けられた。前記2台の受信機からの誤り
パルスを競合計数する競合計数手段と、該競合計数手段
の入力側及び出力側に設けられた。各子局のバーストタ
イミング信号によシ開閉する第1及び第2のゲート手段
と、前記2台の受信機からの復調信号を受け、いずれか
一方を出力する信号切受信機からの復調信号のうちいず
れか誤り率の少ない側の信号が選択されるように信号切
替器を制御するようにしたことを特徴とするスペースダ
イパーシティ受信装置。
[Claims] 1. A communication network is formed by a plurality of slave stations and one master station, and each slave station transmits data to the master station during the time slot assigned to it, and the master station In a space diversity receiving device provided in a master station in a time-division multidirectional communication system that receives burst signals from a slave station, the space diversity receiving device includes a first receiver having a main antenna, and a sub-antenna. a second receiver comprising a second receiver, and the first and second receivers each have a second receiver. demodulation means for demodulating the input signal from the antenna; and detection means for detecting a code error in a demodulated signal and generating an error pulse, and the space diversity receiving device was further provided for each slave station requiring space diversity. A competition counting means for competitively counting error pulses from the two receivers, and an input side and an output side of the competition counting means were provided. first and second gate means that open and close according to the burst timing signal of each slave station; A space diversity receiving device characterized in that a signal switch is controlled so that one of the signals having a lower error rate is selected.
JP57084953A 1982-05-21 1982-05-21 Space diversity receiver Granted JPS58202642A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP57084953A JPS58202642A (en) 1982-05-21 1982-05-21 Space diversity receiver
US06/494,116 US4530087A (en) 1982-05-21 1983-05-13 Space diversity receiving system for multi-direction time division multiplex communication
DE8383105029T DE3362522D1 (en) 1982-05-21 1983-05-20 Space diversity receiving system for multi-direction time division multiplex communication
AU14819/83A AU561492B2 (en) 1982-05-21 1983-05-20 Tdm space diversity system
CA000428598A CA1203646A (en) 1982-05-21 1983-05-20 Space diversity receiving system for multi-direction time division multiplex communication
EP83105029A EP0095165B1 (en) 1982-05-21 1983-05-20 Space diversity receiving system for multi-direction time division multiplex communication

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57084953A JPS58202642A (en) 1982-05-21 1982-05-21 Space diversity receiver

Publications (2)

Publication Number Publication Date
JPS58202642A true JPS58202642A (en) 1983-11-25
JPS6343027B2 JPS6343027B2 (en) 1988-08-26

Family

ID=13844993

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57084953A Granted JPS58202642A (en) 1982-05-21 1982-05-21 Space diversity receiver

Country Status (6)

Country Link
US (1) US4530087A (en)
EP (1) EP0095165B1 (en)
JP (1) JPS58202642A (en)
AU (1) AU561492B2 (en)
CA (1) CA1203646A (en)
DE (1) DE3362522D1 (en)

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JPS60214641A (en) * 1984-04-10 1985-10-26 Nec Corp Space diversity communication system
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Also Published As

Publication number Publication date
EP0095165B1 (en) 1986-03-12
EP0095165A3 (en) 1984-03-21
US4530087A (en) 1985-07-16
AU1481983A (en) 1983-11-24
DE3362522D1 (en) 1986-04-17
AU561492B2 (en) 1987-05-07
CA1203646A (en) 1986-04-22
EP0095165A2 (en) 1983-11-30
JPS6343027B2 (en) 1988-08-26

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